CN101749119A - 涡轮机入口空气热泵型系统 - Google Patents
涡轮机入口空气热泵型系统 Download PDFInfo
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- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F01K27/00—Plants for converting heat or fluid energy into mechanical energy, not otherwise provided for
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
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Abstract
本发明涉及一种用于涡轮压缩机(20)的入口空气的加热和冷却系统(100)。加热和冷却系统(100)可包括热能存储罐充填回路(190)、与热能存储罐充填回路(190)连通的冷却回路(200),以及与冷却回路(200)和涡轮压缩机(20)的入口空气连通的加热回路(210)。
Description
技术领域
本发明大体涉及燃气轮机发动机,且更具体地涉及同时对涡轮机入口空气提供加热且供应冷却水以充填热能存储罐的涡轮机入口空气热泵型系统。
背景技术
空气冷却系统通常与燃气轮机一起使用,以冷却入口空气温度。取决于环境温度,与燃气轮机发动机一起使用冷却系统可使总功率输出提高较大的百分比。特别地,在一个宽的温度范围上,燃气轮机的功率输出几乎与入口空气温度成反比。例如,已知的燃气轮机在约83华氏度(约28.3摄氏度)的环境温度下仅可产生154兆瓦的功率,但是在约50华氏度(约10摄氏度)的环境温度下可产生171.2兆瓦的功率,提高了超过约百分之十一。同样,可以运行冷却系统,以在更冷的环境温度中用废热来调和冷的入口空气,以便为燃气轮机提供有效率的部分负载操作。
在一年中具有较大的昼夜温度变动的地点或时间,入口空气加热可用于在夜间的部分负载操作或防冻控制,同时冷却可用于白天的有效率操作。但是,加热和冷却操作两者通常涉及外部能源。因此,此附加的功率消耗可能会在某种程度上影响总的涡轮机输出和效率。
因此需要改进的燃气轮机入口空气加热和冷却系统。这种加热和冷却系统应该提供燃气轮机入口空气温度的提前加热和冷却,同时提高总的系统输出和效率。
发明内容
本申请描述了一种用于涡轮压缩机的入口空气的加热和冷却系统。该加热和冷却系统可包括热能存储罐充填回路、与热能存储罐充填回路连通的冷却回路,以及与冷却回路和涡轮压缩机的入口空气连通的加热回路。
本申请进一步描述了一种将用于压缩机入口的入口空气加热和冷却系统作为热泵来操作的方法。该方法可包括步骤:操作冷却器,以充填热能存储罐;将来自冷却器的废热引导到热交换器;在热交换器中加热与压缩机入口和冷却器的废热连通的流体;以及用冷却器的废热来加热压缩机周围的入口空气。
本申请进一步描述了一种用于燃气轮机压缩机的入口空气的加热和冷却系统。该加热和冷却系统可包括具有热能存储罐和冷却蒸发器的热能存储罐充填回路。冷却回路可与热能存储罐充填回路连通。冷却回路可包括冷却冷凝器和热回收型热交换器。加热回路可与冷却回路和燃气轮机压缩机的入口空气连通。加热回路可包括设置在涡轮压缩机周围且与热回收型热交换器连通的流体螺旋管(coil)。
在结合多个附图和权利要求书阅读以下详细说明之后,对于本领域的技术人员,本申请的这些和其它特征将变得清楚。
附图说明
图1是具有空气冷却系统的燃气轮机发动机的示意图。
图2是构造成作为如本文所述的入口空气热泵型系统操作的燃气轮机入口空气加热和冷却系统的示意图。部件列表10 燃气轮机发动机20 压缩机30 燃烧器40 涡轮机50 外部负载60 入口空气加热和冷却系统70 冷/热水螺旋管100 涡轮机入口空气加热和冷却系统110 冷/热水螺旋管120 水冷却器125 初级水泵130 蒸发器140 冷凝器150 冷却塔160 冷凝器水泵170 热回收型热交换器175 次级水泵180 热能存储罐181 顶部182 底部190 热能存储罐充填回路200 冷却回路210 加热回路
具体实施方式
现在参看附图,其中在多个附图中,相同的数字始终指示相同的元件,图1显示了燃气轮机发动机10的示意图。如所知道的,燃气轮机发动机10可包括压缩机20,用以压缩进入气流。压缩机20将压缩气流输送到燃烧器30。燃烧器30使压缩气流与燃料流混合,且点燃混合物。(尽管只显示了单个燃烧器30,但是燃气轮机发动机10可包括任何数量的燃烧器30)。然后热的燃烧气体被输送到涡轮机40。涡轮机40驱动压缩机20和外部负载50,例如发电机等。燃气轮机发动机10可使用天然气、各种类型的合成气和其它燃料。在本文中,燃气轮机发动机10可使用其它构造和构件。
在此实例中,燃气轮机发动机10进一步包括入口空气加热和冷却系统60。入口空气加热和冷却系统60可设置在压缩机20周围,且将进入气流加热或冷却到期望的温度。入口空气加热和冷却系统60包括冷/热水螺旋管70。热或冷水流过螺旋管70,且与进入气流交换热。在那里,入口空气加热和冷却系统60可使用任何类型的热交换装置。如上所述,冷水大体可由制冷设备提供,而热水可通过系统废热提供或从另外的源提供。
重要的是注意,术语“热”、“温”、“冷”和“凉”是以相对意义来使用的。在本文中,不意图限制可应用的温度范围。
图2示出了如本文所描述的完整的燃气轮机入口空气加热和冷却系统100。燃气轮机入口空气加热和冷却系统100可与任何数量的燃气轮机发动机10一起使用。如上所述,冷/热水螺旋管110可设置在各燃气轮机发动机10的压缩机20周围。冷/热水螺旋管110通过流过其中的水流来加热或冷却入口空气,如上所述。本文可使用其它类型的热交换装置。
在冷却模式中,冷/热水螺旋管110可与水冷却器120连通。水冷却器120可为机械式冷却器、吸收式冷却器或任何传统类型的冷却装置。如所知道的,水冷却器120将冷水提供给冷/热水螺旋管110,在冷/热水螺旋管110中,与进入气流交换热。在交换热之后,现在较温的水一般回到水冷却器120。冷/热水螺旋管110可通过初级水泵125与水冷却器120连通。可使用任何数量的水冷却器120和初级水泵125。
各个水冷却器120大体包括蒸发器130和冷凝器140。用于冷却冷凝器140的冷却水可由冷却塔150通过一个或多个冷凝器水泵160来提供。本文可使用其它类型的水源。如所知道的,冷却塔150可起散热器或热源的作用,这取决于总的系统热平衡。本文可使用其它类型的热交换装置。
还可将温水提供给冷/热水螺旋管110。温水可通过废热或外部源来提供。在此实例中,可使用热回收型热交换器170。本文可使用任何类型的热交换装置。来自冷却器120的冷凝器140的温水在回到冷却塔150的途中可通过热回收型热交换器170,且与处于与冷/热水螺旋管110连通的回路交换热,这将在下面更加详细地描述。其它废热源也可与热回收型热交换器170一起使用,即从底循环、发电机排出的热、润滑油废热或任何其它热源。热回收型热交换器170可通过次级水泵175与冷/热水螺旋管110连通。可使用任何数量的次级水泵175。
入口空气加热和冷却系统100还可包括热能存储罐180。热能存储罐180可为传统的分层水热存储系统。本文还可使用其它类型的液体。温水上升到罐180的顶部部分,同时冷却水沉到罐180的底部部分182。本文可使用其它类型的热存储系统。本文可使用任何数量的热能存储罐180。
在热泵模式中,入口空气加热和冷却系统100可包括一定量的热回路。第一回路可为热能存储罐充填回路190。热能存储罐充填回路190可通过初级水泵125使热能存储罐180的顶部181与水冷却器120的蒸发器130连接。然后冷却水可直接流回到热能存储罐180的底部182。因此冷却水可存储在热能存储罐180中以供后面使用。例如,可在冷/热水螺旋管110中使用冷却水,以在白天提供入口空气冷却。
入口空气加热和冷却系统100还可包括热源回路或冷却回路200。冷却回路200可通过冷凝器水泵160来包括水冷却器120的冷凝器140、热回收型热交换器170和冷却塔150。冷水可从冷却塔150泵送到水冷却器120的冷凝器140,以在那里进行热交换。然后添加到来自冷凝器140的水流的废热可在回到冷却塔150之前在热回收型热交换器170中进行交换,这将在下面进行更详细的描述。
入口空气加热和冷却系统100可进一步包括加热回路210。加热回路210可通过次级水泵175使冷/热水螺旋管110与热回收型热交换器170连接。因此来自水冷却器120的冷凝器140的废热可在热回收型热交换器170中进行交换,且提供给冷/热水螺旋管110,以便加热压缩机20周围的进入气流。
因此入口空气加热和冷却系统100可对压缩机130的入口提供加热,且同时对热能存储罐180供应冷却水以供后面使用。可将来自水冷却器120的冷凝器140的废热提供给冷/热水螺旋管110,以便:提供总的燃气轮机发动机10的部分负载控制;对压缩机20提供防冻,而不是使用入口排热;提供冷/热水螺旋管110的防冻,而不使用防冻剂;以及代替传统的入口壳体除冰技术提供入口过滤器的防冻。因此,当入口热对部分负载或防冻控制有用时,可在寒冷的夜间使用在此热泵型模式中的入口空气加热和冷却系统100,同时产生供白天使用的冷却水。因此入口空气加热和冷却系统100提供入口空气加热,而不需要消耗额外能量用于获得有效率的部分负载。这样,可降低附加的功率消耗,同时可提高总的能量产生。
显而易见的是,前述仅涉及本申请的某些实施例,且在不脱离由权利要求书及其等效物限定的本发明的总体精神和范围的情况下,可由本领域的技术人员进行许多改变和修改。
Claims (10)
1.一种用于燃气涡轮压缩机(20)的入口空气的加热和冷却系统(100),包括:
热能存储罐充填回路(190);
与所述热能存储罐充填回路(190)连通的冷却回路(200);以及
与所述冷却回路(200)和所述涡轮压缩机(20)的入口空气连通的加热回路(210)。
2.根据权利要求1所述的用于入口空气的加热和冷却系统(100),其特征在于,所述加热回路(210)包括设置在所述燃气涡轮压缩机(20)周围且与所述入口空气连通的流体螺旋管(110)。
3.根据权利要求1所述的用于入口空气的加热和冷却系统(100),其特征在于,所述加热和冷却系统(100)还包括一个或多个冷却器(120)。
4.根据权利要求3所述的用于入口空气的加热和冷却系统(100),其特征在于,所述热能存储罐充填回路(200)包括一个或多个冷却蒸发器(130)。
5.根据权利要求3所述的用于入口空气的加热和冷却系统(100),其特征在于,所述冷却回路(200)包括一个或多个冷却冷凝器(140)。
6.根据权利要求1所述的用于入口空气的加热和冷却系统(100),其特征在于,所述冷却回路(200)包括冷却塔(150)。
7.根据权利要求1所述的用于入口空气的加热和冷却系统(100),其特征在于,所述加热和冷却系统(100)还包括热回收型热交换器(170)。
8.根据权利要求7所述的用于入口空气的加热和冷却系统(100),其特征在于,所述冷却回路(200)与所述热回收型热交换器(170)连通。
9.根据权利要求7所述的用于入口空气的加热和冷却系统(100),其特征在于,所述加热回路(210)与所述热回收型热交换器(170)连通。
10.一种将用于压缩机入口(20)的入口空气加热和冷却系统(100)作为热泵来操作的方法,包括:
操作冷却器(120),以充填热能存储罐(180);
将来自所述冷却器(120)的废热引导到热交换器(170);
在所述热交换器(170)中加热与所述压缩机入口(20)和所述冷却器(120)的所述废热连通的流体;以及
用所述冷却器(120)的所述废热来加热所述压缩机(20)周围的入口空气。
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US12/332,383 US9470149B2 (en) | 2008-12-11 | 2008-12-11 | Turbine inlet air heat pump-type system |
US12/332383 | 2008-12-11 |
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EP (1) | EP2343437A1 (zh) |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103032175A (zh) * | 2011-10-05 | 2013-04-10 | 通用电气公司 | 加热燃气涡轮入口的方法 |
CN103089447A (zh) * | 2011-11-08 | 2013-05-08 | 通用电气公司 | 进气加热系统 |
CN108798902A (zh) * | 2017-04-27 | 2018-11-13 | 通用电气公司 | 具有蓄热系统的中间冷却的涡轮机 |
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Also Published As
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US20100146981A1 (en) | 2010-06-17 |
AU2009245881A1 (en) | 2010-07-01 |
CA2686360A1 (en) | 2010-06-11 |
US9470149B2 (en) | 2016-10-18 |
EP2343437A1 (en) | 2011-07-13 |
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